Modeling of primary breakup considering turbulent nozzle flow, internal turbulence and surface instability of liquid jet using turbulence decay theory

IF 2.2 4区 工程技术 Q2 ENGINEERING, MECHANICAL International Journal of Engine Research Pub Date : 2024-03-04 DOI:10.1177/14680874241233795
Dai Matsuda, Ippei Kimura, Eriko Matsumura, Jiro Senda
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Abstract

In heat engines utilizing fuel injection, the processes of atomization and spray formation have a significant impact on the combustion process, thereby determining both efficiency and emission characteristics. Accurate prediction and control of spray formation in fuel injection systems play a key role in improving the efficiency and environmental performance of thermal engines, especially with the emergence of carbon-neutral fuels. To achieve accurate prediction of spray mixture formation, it is imperative to refine the atomization model for the liquid jet within numerical simulations. This requires a phenomenological representation of the atomization process that avoids reliance on computational constants obtained from spray experimental results. Consequently, the present study attempts to mathematically model the turbulent nozzle flow and liquid jet atomization process, leading to the development of a novel primary breakup model. The construction of the primary breakup model involves an analysis of the turbulence at the nozzle inlet. By merging this turbulence with the turbulence resulting from wall shear flow within the nozzle, the model provides insight into the internal turbulence and surface instability of the liquid jet, encompassing the turbulence spectrum. Consequently, the influence of nozzle length on the turbulent flow within the nozzle can be understood, and the droplet formation characteristics of the liquid jet can be predicted along with its multi-wavelength dispersion characteristics. The model effectively captures the experimental results in terms of breakup length and droplet dispersion characteristics, thus adding a higher level of accuracy to numerical simulations. Ultimately, the in-depth study of this model, coupled with its comparison with experimental results, enhances the understanding of the liquid jet atomization process.
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利用湍流衰减理论建立考虑到湍流喷嘴流动、内部湍流和液体射流表面不稳定性的一次破裂模型
在使用燃料喷射的热力发动机中,雾化和喷雾形成过程对燃烧过程有重大影响,从而决定了效率和排放特性。准确预测和控制燃油喷射系统中的喷雾形成,对于提高热力发动机的效率和环保性能起着关键作用,特别是在碳中性燃料出现的情况下。要实现喷雾混合物形成的精确预测,必须在数值模拟中完善液体射流的雾化模型。这就要求对雾化过程进行现象描述,避免依赖从喷雾实验结果中获得的计算常数。因此,本研究尝试对湍流喷嘴流动和液体射流雾化过程进行数学建模,从而开发出一种新型的一次破裂模型。初级破裂模型的构建涉及对喷嘴入口处湍流的分析。通过将该湍流与喷嘴内壁剪切流产生的湍流合并,该模型可深入了解液体射流的内部湍流和表面不稳定性,包括湍流频谱。因此,可以理解喷嘴长度对喷嘴内湍流的影响,并预测液体射流的液滴形成特征及其多波长分散特征。该模型有效地捕捉了实验结果中的破裂长度和液滴分散特性,从而提高了数值模拟的精确度。通过对该模型的深入研究以及与实验结果的对比,最终加深了人们对液体射流雾化过程的理解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
International Journal of Engine Research
International Journal of Engine Research 工程技术-工程:机械
CiteScore
6.50
自引率
16.00%
发文量
130
审稿时长
>12 weeks
期刊介绍: The International Journal of Engine Research publishes high quality papers on experimental and analytical studies of engine technology.
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